Pages that link to "Item:Q356984"
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The following pages link to Synthesis of stabilizing spacecraft control based on generalized Ackermann's formula (Q356984):
Displaying 17 items.
- Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators (Q295600) (← links)
- The use of the exact pole placement algorithm for the control of spacecraft motion (Q394076) (← links)
- Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components (Q786105) (← links)
- Application of generalized Butterworth polynomials for stabilization of the equilibrium position of a space station (Q786175) (← links)
- Synthesis of spacecraft covariance controls (Q895307) (← links)
- Asymptotic behavior of solutions of Lorenz-like systems: analytical results and computer error structures (Q1696065) (← links)
- Terminal synthesis of orbital orientation for a spacecraft (Q1745868) (← links)
- Algorithms for the synthesis of observers for nonlinear dynamic systems (Q2017643) (← links)
- Synthesis of decoupling laws for attitude stabilization of a spacecraft (Q2263388) (← links)
- Identification of the position of an equilibrium attitude of the international space station as a problem of stable matrix completion (Q2263414) (← links)
- Modification of the exact pole placement method and its application for the control of spacecraft motion (Q2263439) (← links)
- Delayed feedback stabilization and the Huijberts-Michiels-Nijmeijer problem (Q2358673) (← links)
- (Q3305738) (← links)
- (Q3305759) (← links)
- Synthesis and analysis of robust control compensators for Space descent & landing (Q4684586) (← links)
- (Q5006780) (← links)
- On analytic solution of the Lyapunov equation in the problem of analysis of a linear discrete dynamic system (Q5871674) (← links)
